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I got the inlet and outlet pressure of Saturn V engines turbopumps here, but I couldn't find the turbopump pressure of the Merlin engine of Falcon 9.

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This might be useful. not a merlin engine.

Inlet = 3.5 bar. Outlet = 75 bar.

enter image description here

enter image description here

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    $\begingroup$ Is that the Merlin? The paper says it's a proposed engine. $\endgroup$ – Organic Marble Apr 20 at 13:59
  • $\begingroup$ I don't think so. It's some engine the author is designing. $\endgroup$ – Organic Marble Apr 21 at 11:11

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